Bulk amorphous metal magnetic components for electric motors

ABSTRACT

A high efficiency electric motor has a generally polyhedrally shaped bulk amorphous metal magnetic component in which a plurality of layers of amorphous metal strips are laminated together to form a generally three-dimensional part having the shape of a polyhedron. The bulk amorphous metal magnetic component may include an arcuate surface, and preferably includes two arcuate surfaces that are disposed opposite to each other. The magnetic component is operable at frequencies ranging from between approximately 60 Hz and 20,000 Hz and exhibits (i) a core-loss of less than or approximately equal to 1 watt-per-kilogram of amorphous metal material when operated at a frequency of approximately 60 Hz and at a flux density of approximately 1.4 Tesla (T); (ii) a core-loss of less than or approximately equal to 20 watts-per-kilogram of amorphous metal material when operated at a frequency of approximately 1000 Hz and at a flux density of approximately 1.4 T and (iii) a core-loss of less than or approximately equal to 70 watt-per-kilogram of amorphous metal material when operated at a frequency of approximately 20,000 Hz and at a flux density of approximately 0.30 T. Performance characteristics of the bulk amorphous metal magnetic component of the present invention are significantly better when compared to silicon-steel components operated over the same frequency range.

BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention relates to amorphous metal magnetic components, and more particularly, to a high efficiency electric motor having a generally polyhedrally shaped bulk amorphous metal magnetic component.

2. Description of the Prior Art

An electric motor typically contains magnetic components made from a plurality of stacked laminations of non-oriented electrical steel. In variable reluctance motors and eddy current motors, the stators are made from stacked laminations. Both the stator and the rotor are made from stacked laminations in squirrel cage motors, reluctance synchronous motors and switched reluctance motors. Each lamination is typically formed by stamping, punching or cutting the mechanically soft, non-oriented electrical steel into the desired shape. The formal laminations are then stacked and bound to form the rotor or stator.

Although amorphous metals offer superior magnetic performance when compared to non-oriented electrical steels, they have long been considered unsuitable for use in bulk magnetic components such as the rotors and stators of electric motors due to certain physical properties and the corresponding fabricating limitations. For example, amorphous metals are thinner and harder than non-oriented steel and consequently cause fabrication tools and dies to wear more rapidly. The resulting increase in the tooling and manufacturing costs makes fabricating bulk amorphous metal magnetic components using such techniques commercially impractical. The thinness of amorphous metals also translates into an increased number of laminations in the assembled components, further increasing the total cost of an amorphous metal rotor or stator magnet assembly.

Amorphous metal is typically supplied in a thin continuous ribbon having a uniform ribbon width. However, amorphous metal is a very hard material, making it very difficult to cut or form easily, and once annealed to achieve peak magnetic properties, becomes very brittle. This makes it difficult and expensive to use conventional approaches to construct a bulk amorphous metal magnetic component. The brittleness of amorphous metal may also cause concern for the durability of the bulk magnetic component in an application such as an electric motor.

Another problem with bulk amorphous metal magnetic components is that the magnetic permeability of amorphous metal material is reduced when it is subjected to physical stresses. This reduced permeability may be considerable depending upon the intensity of the stresses on the amorphous metal material. As a bulk amorphous metal magnetic component is subjected to stresses, the efficiency at which the core directs or focuses magnetic flux is reduced resulting in higher magnetic losses, increased heat production, and reduced power. This stress sensitivity, due to the magnetostrictive nature of the amorphous metal, may be caused by stresses resulting from magnetic and mechanical forces during the operation of the electric motor, mechanical stresses resulting from mechanical clamping or otherwise fixing the bulk amorphous metal magnetic components in place, or internal stresses caused by the thermal expansion and/or expansion due to magnetic saturation of the amorphous metal material.

SUMMARY OF THE INVENTION

The present invention provides a bulk amorphous metal magnetic component having the shape of a polyhedron and being comprised of a plurality of layers of amorphous metal strips for use in highly efficient electric motors. Also provided by the present invention is a method for making a bulk amorphous metal magnetic component. The magnetic component is operable at frequencies ranging from about 60 Hz to 20,000 Hz and exhibits improved performance characteristics when compared to silicon-steel magnetic components operated over the same frequency range. More specifically, a magnetic component constructed in accordance with the present invention will have (i) a core-loss of less than or approximately equal to 1 watt-per-kilogram of amorphous metal material when operated at a frequency of approximately 60 Hz and at a flux density of approximately 1.4 Tesla (T); (ii) a core-loss of less than or approximately equal to 20 watts-per-kilogram of amorphous metal material when operated at a frequency of approximately 1000 Hz and at a flux density of approximately 1.4 T, and (iii) a core-loss of less than or approximately equal to 70 watt-per-kilogram of amorphous metal material when operated at a frequency of approximately 20,000 Hz and at a flux density of approximately 0.30 T.

In a first embodiment of the present invention, a bulk amorphous metal magnetic component comprises a plurality of substantially similarly shaped layers of amorphous metal strips laminated together to form a polyhedrally shaped part.

The present invention also provides a method of constructing a bulk amorphous metal magnetic component. In accordance with a first embodiment of the inventive method, amorphous metal strip material is cut to form a plurality of cut strips having a predetermined length. The cut strips are stacked to form a bar of stacked amorphous metal strip material and annealed. The annealed, stacked bar is impregnated with an epoxy resin and cured. The stacked bar is then cut at predetermined lengths to provide a plurality of polyhedrally shaped magnetic components having a predetermined three-dimensional geometry. The preferred amorphous metal material has a composition defined essentially by the formula Fe₈₀B₁₁Si₉.

In accordance with a second embodiment of the method of the present invention, an amorphous metal ribbon is wound about a mandrel to form a generally rectangular core having generally radiused corners. The generally rectangular core is then annealed, impregnated with epoxy resin and cured. The short sides of the rectangular core are then cut to form two magnetic components having a predetermined three-dimensional geometry that is the approximate size and shape of said short sides of said generally rectangular core. The radiused corners are removed from the long sides of said generally rectangular core and the long sides of said generally rectangular core are cut to form a plurality of polyhedrally shaped magnetic components having the predetermined three-dimensional geometry. The preferred amorphous metal material has a composition defined essentially by the formula Fe₈₀B₁₁Si₉.

The present invention is also directed to a bulk amorphous metal component constructed in accordance with the above-described methods.

Construction of bulk amorphous metal magnetic components in accordance with the present invention is especially suited for amorphous metal stators or stator components in highly efficient, variable reluctance motors and eddy current motors. Similarly, bulk amorphous metal components may be used as both the rotor and the stator in squirrel cage motors, reluctance synchronous motors and switched reluctance motors. The advantages recognized by the present invention include simplified manufacturing and reduced manufacturing time, reduced stresses (i.e., magnetostrictive) encountered during construction of bulk amorphous metal components, and optimized performance of the finished amorphous metal magnetic component.

BRIEF DESCRIPTION OF THE DRAWINGS

The invention will be more fully understood and further advantages will become apparent when reference is had to the following detailed description of the preferred embodiments of the invention and the accompanying drawings, wherein like reference numeral denote similar elements throughout the several views and in which:

FIG. 1 is a perspective view of a bulk amorphous metal magnetic component in the shape of a three-dimensional rectangle constructed in accordance with the present invention;

FIG. 2A is a perspective view of a bulk amorphous metal magnetic component having the shape of a prism and constructed in accordance with the present invention;

FIG. 2B is a perspective view of a bulk amorphous metal magnetic component having oppositely disposed arcuate surfaces and constructed in accordance with the present invention;

FIG. 2C is a top view of a stator for an electric motor constructed from six prism-shaped components as depicted in FIG. 2A and six arcuate components as depicted in FIG. 2B;

FIG. 3A is a perspective view of a bulk amorphous metal magnetic stator for an electric motor constructed in accordance with the present invention;

FIG. 3B is a perspective view of a bulk amorphous metal magnetic rotor for an electric motors constructed in accordance with the present invention;

FIG. 3C is a top view of the stator and rotor for an electric motor constructed from the stator of FIG. 3A and the rotor of FIG. 3B;

FIG. 4 is a side view of a coil of amorphous metal strip positioned to be cut and stacked in accordance with the present invention;

FIG. 5 is a perspective view of a bar of amorphous metal strips showing the cut lines to produce a plurality of generally prism-shaped magnetic components in accordance with the present invention;

FIG. 6 is a side view of a coil of amorphous metal strip which is being wound about a mandrel to form a generally rectangular core in accordance with the present invention; and

FIG. 7 is a perspective view of a generally rectangular amorphous metal core showing the cut lines to produce a plurality of generally prism-shaped magnetic components formed in accordance with the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

The present invention is directed to high efficiency motors constructed using bulk amorphous metal components such as, for example stators, rotors, and component parts for stators and rotors. Generally polyhedrally shaped bulk amorphous metal components are constructed in accordance with the present invention having various geometries including, but not limited to, rectangular, square, prism. In addition, any of the previously mentioned geometric shapes may include at least one arcuate surface, and preferably two oppositely disposed arcuate surfaces to form a generally curved or arcuate bulk amorphous metal component. Furthermore, complete stators and rotors may be constructed as a bulk amorphous metal component in accordance with the present invention. Those stators and rotors may have either a unitary construction or they may be formed from a plurality of pieces which collectively form the completed component. Alternatively, a stator and/or rotor may be a composite structure comprised entirely of amorphous metal parts or a combination of amorphous metal parts with other magnetic materials.

Referring now to the drawings in detail, FIG. 1 depicts a generally polyhedrally shaped bulk amorphous metal component 10. As used herein, the term polyhedron refers to a multi-faced or sided solid. This includes, but is not limited to, three-dimensional rectangles, squares, trapezoids, and prisms. In addition, any of the previously mentioned geometric shapes may include at least one, and preferably two, arcuate surfaces or sides that are disposed opposite each other to form a generally arcuately shaped component. The magnetic component 10 depicted in FIG. 1 is comprised of a plurality of substantially similarly shaped layers of amorphous metal strip material 20 that are laminated together and annealed. In a preferred embodiment, a three-dimensional magnetic component 10 constructed in accordance with the present invention and having a flux density of approximately 1.4 Tesla (T) will have (i) a core-loss of less than or approximately equal to 1 watt-per-kilogram of amorphous metal material when operated at a frequency of approximately 60 Hz and at a flux density of approximately 1.4 Tesla (T); (ii) a core-loss of less than or approximately equal to 20 watts-per-kilogram of amorphous metal material when operated at a frequency of approximately 1000 Hz and at a flux density of approximately 1.4 T, and (iii) a core-loss of less than or approximately equal to 70 watt-per-kilogram of amorphous metal material when operated at a frequency of approximately 20,000 Hz and at a flux density of approximately 0.30 T. These performance values apply to the various embodiments of the present invention, regardless of the specific geometry of the bulk amorphous metal component.

The magnetic component 100 depicted in FIG. 2A is generally prism-shaped and preferably includes five (5) sides 110 or surfaces. The pentagonnally-shaped polyhedron component 100 is comprised of a plurality of layers of amorphous metal strip material 20 that are each substantially the same size and shape. The strip material 20 is stacked, laminated together and then annealed.

The magnetic component 200 depicted in FIG. 2B includes at least one, and preferably two oppositely disposed arcuate surfaces 210. The arcuately-shaped component 200 is comprised of a plurality of layers of amorphous metal strip material 20 that are each substantially the same size and shape and that are stacked, laminated together, and annealed.

The bulk amorphous metal magnetic component 300 depicted in FIG. 2C may be used as a stator for a radial gap electric motor and is comprised of six pieces of magnetic component 100 and six pieces of magnetic component 200.

The bulk amorphous metal magnetic component 400 depicted in FIG. 3A is generally circular and includes a plurality of generally rectangular teeth 410 that extend radially inward toward the center of the circular component 400. The component 400 is comprised of a plurality of layers of amorphous metal strip material 20 that are each substantially the same size and shape and that are stacked, laminated together, and then annealed. A bulk amorphous metal component constructed in accordance with the embodiment of FIG. 3A may be used as a stator in a radial air gap electric motor.

The bulk amorphous metal component 500 depicted in FIG. 3B is generally disc-shaped and includes a plurality of generally rectangular teeth 510 that extend radially outward. The component 500 is comprised of a plurality of layers of amorphous metal strip material 20 that are each substantially the same size and shape and that are stacked, laminated together, and then annealed. A bulk amorphous metal component constructed in accordance with the embodiment of FIG. 3B may be used as a rotor in a radial air gap electric motor.

Referring next to FIG. 3C, a stator 400 and rotor 500 are constructed as bulk amorphous metal components in accordance with the present invention and used as part of a high efficiency radial air gap electric motor 600.

The present invention also provides a method of constructing a bulk amorphous metal component. As shown in FIG. 4, a roll 30 of amorphous metal strip material is cut by cutting blades 40 into a plurality of strips 20 having the same shape and size. The strips 20 are stacked to form a bar 50 of stacked amorphous metal strip material. The bar 50 is annealed, impregnated with an epoxy resin and cured. The bar 50 can be cut along the lines 52 depicted in FIG. 5 to produce a plurality of generally trapezoidally-shaped magnetic components 10. The finished magnetic component 10 may be generally rectangular, trapezoidal, square, or other polyhedral shape. The bar 50 may also be cut to produce three dimensional shapes in the form of pentagonal prisms 11, arc-shaped blocks 12. circular-shaped blocks 13 or disc-shaped blocks 14, as shown in FIGS. 2A, 2B, 3A and 3B respectively.

In a second embodiment of the method of the present invention, shown in FIGS. 6 and 7, a bulk amorphous metal magnetic component 10 is formed by winding a single amorphous metal strip 22 or a group of amorphous metal strips 22 around a generally rectangular mandrel 60 to form a generally rectangular wound core 70. The height of the short sides 74 of the core 70 is preferably approximately equal to the desired length of the finished bulk amorphous metal magnetic component 10. The core 70 is annealed, impregnated with an epoxy resin and cured. Two components 10 may be formed by cutting the short sides 74, leaving the radiused corners 76 on the long sides 78. Additional magnetic components 10 may be formed by removing the radiused corners 76 from the long sides 78, and cutting the long sides 78 at a plurality of locations, indicated by the dashed lines 72. In the example illustrated in FIG. 7, the bulk amorphous metal component 10 has a generally rectangular shape, although other shapes are contemplated by the present invention. The wound core 70 may also be cut to produce three dimensional shapes in the form of pentagonal prisms 11, arc-shaped blocks 12, circular-shaped blocks 13 or disc-shaped blocks 14, as shown in FIG. 2A, 2B, 3A and 3B respectively.

Construction in this manner is especially suited for magnetic components such as amorphous metal stator and rotor assemblies in electric motors. Magnetic component manufacturing is simplified and manufacturing time is reduced. Stresses otherwise encountered during the construction of bulk amorphous metal components are minimized. Magnetic performance of the finished components is optimized.

The bulk amorphous metal magnetic component 10 of the present invention can be manufactured using numerous amorphous metal alloys. Generally stated, the alloys suitable for use in the component 10 construction of the present invention are defined by the formula: M₇₀₋₈₅ Y₅₋₂₀ Z₀₋₂₀, subscripts in atom percent, where “M” is at least one of Fe, Ni and Co, “Y” is at least one of B, C and P, and “Z” is at least one of Si, Al and Ge; with the proviso that (i) up to ten (10) atom percent of component “M” can be replaced with at least one of the metallic species Ti, V, Cr, Mn, Cu, Zr, Nb, Mo, Ta and W, and (ii) up to ten (10) atom percent of components (Y+Z) can be replaced by at least one of the non-metallic species In, Sn, Sb and Pb. Highest induction values at low cost are achieved for alloys wherein “M” is iron, “Y” is boron and “Z” is silicon. For this reason, amorphous metal strip composed of iron-boron-silicon alloys is preferred. Most preferred is amorphous metal strip having a composition consisting essentially of about 11 atom percent boron and about 9 atom percent silicon, the balance being iron and incidental impurities. This strip is sold by AlliedSignal Inc. under the trade designation METLAS® alloy 2605SA-1.

The bulk amorphous metal magnetic component 10 of the present invention can be cut from bars 50 of stacked amorphous metal strip or from cores 70 of wound amorphous metal strip using numerous cutting technologies. The component 10 may be cut from the bar 50 or core 70 using a cutting blade or wheel. Alternately, the component 10 may be cut by electro-discharge machining or with a water jet.

Bulk amorphous magnetic components will magnetize and demagnetize more efficiently than components made from other iron-base magnetic metals. When used as the rotor or stator in an electric motor, the bulk amorphous metal component will generate less heat than a comparable component made from another iron-base magnetic metal when the two components are magnetized at identical induction and frequency. The electric motor using the bulk amorphous metal component can therefore be designed to operate 1) at a lower operating temperature; 2) at higher induction to achieve reduced size and weight; or, 3) at higher frequency to achieve reduced size and weight, or to achieve superior motion control, when compared to electric motors using components made from other iron-base magnetic metals.

The following example is presented to provide a more complete understanding of the invention. The specific techniques, conditions, materials, proportions and reported data set forth to illustrate the principles and practice of the invention are exemplary and should not be construed as limiting the scope of the invention.

EXAMPLE 1 Preparation And Electro-Magnetic Testing of an Amorphous Metal Rectangular Prism

Fe₈₀B₁₁Si₉ amorphous metal ribbon, approximately 60 mm wide and 0.022 mm thick, was wrapped around a rectangular mandrel or bobbin having dimensions of approximately 25 mm by 90 mm. Approximately 800 wraps of amorphous metal ribbon were wound around the mandrel or bobbin producing a rectangular core form having inner dimensions of approximately 25 mm by 90 mm and a build thickness of approximately 20 mm. The core/bobbin assembly was annealed in a nitrogen atmosphere. The anneal consisted of: 1) heating the assembly up to 365° C.; 2) holding the temperature at approximately 365° C. for approximately 2 hours: and, 3) cooling the assembly to ambient temperature. The rectangular, wound, amorphous metal core was removed from the core/bobbin assembly. The core was vacuum impregnated with an epoxy resin solution. The bobbin was replaced, and the rebuilt, impregnated core/bobbin assembly was cured at 120° C. for approximately 4.5 hours. When fully cured, the core was again removed from the core/bobbin assembly. The resulting rectangular, wound, epoxy bonded, amorphous metal core weighed approximately 2100 g.

A rectangular prism 60 mm long by 40 mm wide by 20 mm thick (approximately 800 layers) was cut from the epoxy bonded amorphous metal core with a 1.5 mm thick cutting blade. The cut surfaces of the rectangular prism and the remaining section of the core were etched in a nitric acid/water solution and cleaned in an ammonium hydroxide/water solution.

The remaining section of the core was etched in a nitric acid/water solution and cleaned in an ammonium hydroxide/water solution. The rectangular prism and the remaining section of the core were then reassembled into a full, cut core form. Primary and secondary electrical windings were fixed to the remaining section of the core. The cut core form was electrically tested at 60 Hz, 1,000 Hz, 5,000 Hz and 20,000 Hz and compared to catalogue values for other ferromagnetic materials in similar test configurations [National Arnold Magnetics, 17030 Muskrat Avenue, Adelanto, Calif. 92301 (1995)]. The results are compiled below in Tables 1, 2, 3 and 4.

TABLE 1 Core Loss @ 60 Hz (W/kg) Material Crystalline Crystalline Crystalline Crystalline Fe—3% Si Fe—3% Si Fe—3% Si Fe—3% Si Amorphous (25 μm) (50 μm) 175 (μm) (275 μm) Flux Fe₈₀B₁₁Si₉ National-Arnold National-Arnold National-Arnold National-Arnold Density (22 μm) Magnetics Silectron Magnetics Silectron Magnetics Silectron Magnetics Silectron 0.3 T 0.10 0.2 0.1 0.1  0.06 0.7 T 0.33 0.9 0.5 0.4 0.3 0.8 T 1.2 0.7 0.6 0.4 1.0 T 1.9 1.0 0.8 0.6 1.1 T 0.59 1.2 T 2.6 1,5 1.1 0.8 1.3 T 0.75 1.4 T 0.85 3.3 1.9 1.5 1.1

TABLE 2 Core Loss @ 1,000 Hz, (W/kg) Material Crystalline Crystalline Crystalline Crystalline Fe—3% Si Fe—3% Si Fe—3% Si Fe—3% Si Amorphous (25 μm) (50 μm) 175 (μm) (275 μm) Flux Fe₈₀B₁₁Si₉ National-Arnold National-Arnold National-Arnold National-Arnold Density (22 μm) Magnetics Silectron Magnetics Silectron Magnetics Silectron Magnetics Silectron 0.3 T  1.92 2.4 2.0 3.4 5.0 0.5 T  4.27 6.6 5.5 8.8 12 0.7 T  6.94 13 9.0 18 24 0.9 T  9.92 20 17 28 41 1.0 T 11.51 24 20 31 46 1.1 T 13.46 1.2 T 15.77 33 28 1.3 T 17.53 1.4 T 19.67 44 35

TABLE 3 Core Loss @ 5,000 Hz (W/kg) Material Crystalline Crystalline Crystalline Fe—3% Si Fe—3% Si Fe—3% Si Amorphous (25 μm) (50 μm) (175 μm) Fe₈₀B₁₁Si₉ National-Arnold National-Arnold National-Arnold Flux Density (22 μm) Magnetics-Silectron Magnetics-Silectron Magnetics-Silectron 0.04 T 0.25 0.33 0.33 1.3 0.06 T 0.52 0.83 0.80 2.5 0.08 T 0.88 1.4 1.7 4.4 0.10 T 1.35 2.2 2.1 6.6 0.20 T 5 8.8 8.6 24 0.30 T 10 18.7 18.7 48

TABLE 4 Core Loss @ 20,000 Hz (W/kg) Material Crystalline Crystalline Crystalline Fe—3% Si Fe—3% Si Fe—3% Si Amorphous (25 μm) (50 μm) (175 μm) Fe₈₀B₁₁Si₉ National-Arnold National-Arnold National-Arnold Flux Density (22 μm) Magnetics-Silectron Magnetics-Silectron Magnetics-Silectron 0.04 T 1.8 2.4 2.8 16 0.06 T 3.7 5.5 7.0 33 0.08 T 6.1 9.9 12 53 0.10 T 9.2 15 20 88 0.20 T 35 57 82 0.30 T 70 130

EXAMPLE 2 Preparation of an Amorphous Metal Trapezoidal Prism

Fe₈₀B₁₁Si₉ amorphous metal ribbon, approximately 48 mm wide and 0.022 mm thick, was cut into lengths of approximately 300 mm. Approximately 3,800 layers of the cut amorphous metal ribbon were stacked to form a bar approximately 48 mm wide and 300 mm long, with a build thickness of approximately 96 mm. The bar was annealed in a nitrogen atmosphere. The anneal consisted of: 1) heating the bar up to 365° C.; 2) holding the temperature at approximately 365° C. for approximately 2 hours; and, 3) cooling the bar to ambient temperature. The bar was vacuum impregnated with an epoxy resin solution and cured at 120° C. for approximately 4.5 hours. The resulting stacked, epoxy bonded, amorphous metal bar weighed approximately 9000 g.

A trapezoidal prism was cut from the stacked, epoxy bonded amorphous metal bar with a 1.5 mm thick cutting blade. The trapezoid-shaped face of the prism had bases of 52 and 62 mm and height of 48 mm. The trapezoidal prism was 96 mm (3,800 layers) thick. The cut surfaces of the trapezoidal prism and the remaining section of the core were etched in a nitric acid/water solution and cleaned in an ammonium hydroxide/water solution.

EXAMPLE 3 Preparation of Polygonal, Bulk Amorphous Metal Components With Arc-Shaped Cross-Sections

Fe₈₁B₁₁Si₉ amorphous metal ribbon, approximately 50 mm wide and 0.022 mm thick, was cut into lengths of approximately 300 mm. Approximately 3,800 layers of the cut amorphous metal ribbon were stacked to form a bar approximately 50 mm wide and 300 mm long, with a build thickness of approximately 96 mm. The bar was annealed in a nitrogen atmosphere. The anneal consisted of: 1) heating the bar up to 365° C.; 2) holding the temperature at approximately 365° C. for approximately 2 hours; and, 3) cooling the bar to ambient temperature. The bar was vacuum impregnated with an epoxy resin solution and cured at 1 20° C. for approximately 4.5 hours. The resulting stacked, epoxy bonded, amorphous metal bar weighed approximately 9200 g.

The stacked, epoxy bonded, amorphous metal bar was cut using electro-discharge machining to form a three-dimensional, arc-shaped block. The outer diameter of the block was approximately 96 mm. The inner diameter of the block was approximately 13 mm. The arc length was approximately 90°. The block thickness was approximately 96 mm.

Fe₈₁B₁₁Si₉ amorphous metal ribbon, approximately 20 mm wide and 0.022 mm thick, was wrapped around a circular mandrel or bobbin having an outer diameter of approximately 19 mm. Approximately 1,200 wraps of amorphous metal ribbon were wound around the mandrel or bobbin producing a circular core form having an inner diameter of approximately 19 mm and an outer diameter of approximately 48 mm. The core had a build thickness of approximately 29 mm. The core was annealed in a nitrogen atmosphere. The anneal consisted of: 1) heating the bar up to 365° C.; 2) holding the temperature at approximately 365° C. for approximately 2 hours; and, 3) cooling the bar to ambient temperature. The core was vacuum impregnated with an epoxy resin solution and cured at 120° C. for approximately 4.5 hours. The resulting wound, epoxy bonded, amorphous metal core weighed approximately 71 g.

The wound, epoxy bonded, amorphous metal core was cut using a water jet to form a semi-circular, three dimensional shaped object. The semi-circular object had an inner diameter of approximately 19 mm, an outer diameter of approximately 48 mm, and a thickness of approximately 20 mm.

The cut surfaces of the polygonal bulk amorphous metal components were etched in a nitric acid/water solution and cleaned in an ammonium hydroxide/water solution.

Having thus described the invention in rather full detail, it will be understood that such detail need not be strictly adhered to but that various changes and modifications may suggest themselves to one skilled in the art, all falling within the scope of the present invention as defined by the subjoined claims. 

What is claimed is:
 1. An electric motor having at least one bulk amorphous metal magnetic component comprising a plurality of substantially similarly shaped layers of amorphous metal strips having a composition defined essentially by the formula Fe₈₀B₁₁Si₉ and laminated together by impregnating the component with an epoxy resin and curing to form a polyhedrally shaped part, said bulk amorphous metal magnetic component having a core-loss of less than or approximately equal to 20 watts-per-kilogram of amorphous metal material when operated at a frequency of approximately 1000 Hz and a flux density of approximately 1.4T.
 2. An electric motor having at least one bulk amorphous metal magnetic component comprising a plurality of substantially similarly shaped layers of amorphous metal strips having a composition defined essentially by the formula Fe₈₀B₁₁Si₉ and laminated together by impregnating the component with an epoxy resin and curing to form a polyhedrally shaped part, said bulk amorphous metal magnetic component having a core-loss of less than or approximately equal to 70 watts-per-kilogram of amorphous metal material when operated at a frequency of approximately 20,000 Hz and a flux density of approximately .30T. 